[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 2nd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 106)
---------------------------------------
Vector Time (GMT): 2012/060/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5167833
20 A = 6768751
55 meter
Y = 1368997
38 meter E =
0024488
Z = -4171819
43 I = 51
35968
XDOT = 1217
704407 Wp = 93
17027
YDOT = -6598
780002 meter/sec RA = 306
56528 deg
ZDOT = -3693
964379 TA = 138
79435
MA = 138
60923
Ha = 220
253 n
mi
Hp = 201
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16954833
34 X = -5162491
96
Y = 4491461
23 feet Y = 1311237
11 meter
Z = -13687071
62 Z = -4196911
39
XDOT = 3995
093200 XDOT = 1309
347063
YDOT = -21649
540689 feet/sec YDOT = -6584
650689 meter/sec
ZDOT = -12119
305705 ZDOT = -3687
825910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17118956
12 X = -5217857
82
Y = -3428146
66 feet Y = -1044899
10 meter
Z = -13790020
99 Z = -4203198
40
XDOT = 12968
192942 XDOT = 3952
705209
YDOT = -16374
524501 feet/sec YDOT = -4990
955068 meter/sec
ZDOT = -12093
618100 ZDOT = -3686
134797
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12060
51138276
00016717 00000-0 10270-3 0 9009
2 25544 51
6426 307
0556 0017472 103
9208 256
3891 15
58634641 1071
Satellite: ISS
Catalog Number: 25544
Epoch time: 12060
51138276 = yrday
fracday
Element set: 900
Inclination: 51
6426 deg
RA of node: 307
0556 deg
Eccentricity:
0017472
Arg of perigee: 103
9208 deg
Mean anomaly: 256
3891 deg
Mean motion: 15
58634641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 107
Checksum: 294
Coasting Arc #2 (Orbit 122)
---------------------------------------
Vector Time (GMT): 2012/061/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3801474
00 A = 6764141
93 meter
Y = 1856440
54 meter E =
0020004
Z = 5261628
84 I = 51
32728
XDOT = -3769
793941 Wp = 107
10944
YDOT = 6694
212698 meter/sec RA = 301
50416 deg
ZDOT = 354
831975 TA = 339
46260
MA = 339
54290
Ha = 220
068 n
mi
Hp = 201
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12472027
57 X = 3754872
87
Y = 6090684
20 feet Y = 1898690
68 meter
Z = 17262561
82 Z = 5279982
73
XDOT = -12368
090359 XDOT = -3846
093468
YDOT = 21962
640085 feet/sec YDOT = 6651
629940 meter/sec
ZDOT = 1164
146900 ZDOT = 336
333039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8588129
40 X = 2617661
84
Y = 10783980
84 feet Y = 3286957
36 meter
Z = 17337639
31 Z = 5284512
46
XDOT = -19773
080152 XDOT = -6026
834830
YDOT = 13961
675029 feet/sec YDOT = 4255
518549 meter/sec
ZDOT = 1087
797107 ZDOT = 331
560558
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12061
53723010
00016717 00000-0 10270-3 0 9019
2 25544 51
6426 301
9066 0017452 107
8337 252
4723 15
58682001 1236
Satellite: ISS
Catalog Number: 25544
Epoch time: 12061
53723010 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 301
9066 deg
Eccentricity:
0017452
Arg of perigee: 107
8337 deg
Mean anomaly: 252
4723 deg
Mean motion: 15
58682001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 123
Checksum: 269
Coasting Arc #3 (Orbit 137)
---------------------------------------
Vector Time (GMT): 2012/062/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1653434
03 A = 6767416
40 meter
Y = -4789361
55 meter E =
0027026
Z = -4513257
30 I = 51
32303
XDOT = 5146
803758 Wp = 110
69345
YDOT = -4721
798092 meter/sec RA = 296
43717 deg
ZDOT = 3131
009793 TA = 190
87611
MA = 190
93466
Ha = 220
087 n
mi
Hp = 201
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5424652
32 X = -1577831
47
Y = -15713128
45 feet Y = -4807428
77 meter
Z = -14807274
61 Z = -4521105
62
XDOT = 16885
839102 XDOT = 5184
011817
YDOT = -15491
463556 feet/sec YDOT = -4664
035164 meter/sec
ZDOT = 10272
341840 ZDOT = 3156
102968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1592312
90 X = 485336
97
Y = -16518209
09 feet Y = -5034750
13 meter
Z = -14839068
30 Z = -4522948
02
XDOT = 20497
543128 XDOT = 6247
651145
YDOT = -7327
628033 feet/sec YDOT = -2233
461025 meter/sec
ZDOT = 10375
559114 ZDOT = 3162
470418
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12062
49894510
00016717 00000-0 10270-3 0 9020
2 25544 51
6424 297
0789 0017307 111
1954 249
1052 15
58693532 1388
Satellite: ISS
Catalog Number: 25544
Epoch time: 12062
49894510 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 297
0789 deg
Eccentricity:
0017307
Arg of perigee: 111
1954 deg
Mean anomaly: 249
1052 deg
Mean motion: 15
58693532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 138
Checksum: 312
Coasting Arc #4 (Orbit 153)
---------------------------------------
Vector Time (GMT): 2012/063/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -732421
78 A = 6774264
84 meter
Y = 6394447
81 meter E =
0031376
Z = 2063540
32 I = 51
33331
XDOT = -5214
883871 Wp = 112
89885
YDOT = 1201
657969 meter/sec RA = 291
39981 deg
ZDOT = -5519
766734 TA = 44
08331
MA = 43
83360
Ha = 220
063 n
mi
Hp = 201
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2402958
58 X = -813895
38
Y = 20979159
49 feet Y = 6385801
99 meter
Z = 6770145
40 Z = 2059784
08
XDOT = -17109
199052 XDOT = -5201
120167
YDOT = 3942
447404 feet/sec YDOT = 1143
418582 meter/sec
ZDOT = -18109
470913 ZDOT = -5545
066583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10534142
74 X = -3210806
71
Y = 18306993
92 feet Y = 5579971
75 meter
Z = 6754259
54 Z = 2058698
31
XDOT = -15838
142610 XDOT = -4827
465867
YDOT = -2327
306181 feet/sec YDOT = -709
362924 meter/sec
ZDOT = -18213
261708 ZDOT = -5551
402169
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12063
52475621
00016717 00000-0 10270-3 0 9034
2 25544 51
6423 291
9296 0017426 114
9846 245
3121 15
58703386 1548
Satellite: ISS
Catalog Number: 25544
Epoch time: 12063
52475621 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 291
9296 deg
Eccentricity:
0017426
Arg of perigee: 114
9846 deg
Mean anomaly: 245
3121 deg
Mean motion: 15
58703386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 154
Checksum: 306
Coasting Arc #5 (Orbit 169)
---------------------------------------
Vector Time (GMT): 2012/064/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2691946
53 A = 6775374
55 meter
Y = -6121490
58 meter E =
0026504
Z = 1069181
45 I = 51
32690
XDOT = 4059
617270 Wp = 91
55731
YDOT = 2831
600638 meter/sec RA = 286
38548 deg
ZDOT = 5864
119955 TA = 280
10954
MA = 280
40844
Ha = 219
849 n
mi
Hp = 201
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8831845
57 X = 2755004
46
Y = -20083630
51 feet Y = -6091034
92 meter
Z = 3507813
17 Z = 1082412
11
XDOT = 13318
954298 XDOT = 3999
166033
YDOT = 9290
028339 feet/sec YDOT = 2876
660174 meter/sec
ZDOT = 19239
238699 ZDOT = 5883
693966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15768623
20 X = 4806276
35
Y = -15241967
12 feet Y = -4645751
58 meter
Z = 3562502
57 Z = 1085850
78
XDOT = 7580
683152 XDOT = 2310
592225
YDOT = 12453
821667 feet/sec YDOT = 3795
924844 meter/sec
ZDOT = 19319
259033 ZDOT = 5888
510153
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12064
55054475
00016717 00000-0 10270-3 0 9049
2 25544 51
6415 286
7799 0017168 119
0067 241
2812 15
58768938 1707
Satellite: ISS
Catalog Number: 25544
Epoch time: 12064
55054475 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 286
7799 deg
Eccentricity:
0017168
Arg of perigee: 119
0067 deg
Mean anomaly: 241
2812 deg
Mean motion: 15
58768938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 170
Checksum: 330
Coasting Arc #6 (Orbit 184)
---------------------------------------
Vector Time (GMT): 2012/065/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3964636
33 A = 6769334
47 meter
Y = 3871871
27 meter E =
0021954
Z = -3899855
53 I = 51
29796
XDOT = -2069
425878 Wp = 109
33817
YDOT = -6171
287500 meter/sec RA = 281
35637 deg
ZDOT = -4049
006580 TA = 118
17645
MA = 117
95451
Ha = 219
727 n
mi
Hp = 201
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13007337
05 X = -3988693
51
Y = 12702989
74 feet Y = 3827401
41 meter
Z = -12794801
60 Z = -3919173
90
XDOT = -6789
454979 XDOT = -1980
594760
YDOT = -20247
006232 feet/sec YDOT = -6193
932770 meter/sec
ZDOT = -13284
142323 ZDOT = -4058
843233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16660416
88 X = -5078095
07
Y = 7137744
21 feet Y = 2175584
43 meter
Z = -12874270
10 Z = -3924077
53
XDOT = 1625
430532 XDOT = 495
431226
YDOT = -20086
656522 feet/sec YDOT = -6122
412908 meter/sec
ZDOT = -13324
013523 ZDOT = -4061
159322
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12065
51220613
00016717 00000-0 10270-3 0 9056
2 25544 51
6404 281
9515 0017041 122
6722 237
6080 15
58761281 1852
Satellite: ISS
Catalog Number: 25544
Epoch time: 12065
51220613 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 281
9515 deg
Eccentricity:
0017041
Arg of perigee: 122
6722 deg
Mean anomaly: 237
6080 deg
Mean motion: 15
58761281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 185
Checksum: 282
Coasting Arc #7 (Orbit 200)
---------------------------------------
Vector Time (GMT): 2012/066/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4260196
87 A = 6763994
71 meter
Y = -412466
26 meter E =
0020237
Z = 5224471
55 I = 51
27512
XDOT = -221
428697 Wp = 124
79802
YDOT = 7646
159194 meter/sec RA = 276
29287 deg
ZDOT = 770
710685 TA = 317
74143
MA = 317
89720
Ha = 219
581 n
mi
Hp = 201
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13977023
86 X = 4239113
75
Y = -1353235
77 feet Y = -364943
41 meter
Z = 17140654
69 Z = 5245115
79
XDOT = -726
472102 XDOT = -310
656992
YDOT = 25085
824126 feet/sec YDOT = 7643
184224 meter/sec
ZDOT = 2528
578363 ZDOT = 769
417436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13479226
23 X = 4108468
16
Y = 3548204
96 feet Y = 1081492
87 meter
Z = 17225306
62 Z = 5250273
46
XDOT = -9146
396927 XDOT = -2787
821783
YDOT = 22285
067166 feet/sec YDOT = 6792
488472 meter/sec
ZDOT = 2522
736154 ZDOT = 768
929980
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12066
53795875
00016717 00000-0 10270-3 0 9067
2 25544 51
6401 276
8017 0017086 126
1933 234
0805 15
58790572 2011
Satellite: ISS
Catalog Number: 25544
Epoch time: 12066
53795875 = yrday
fracday
Element set: 906
Inclination: 51
6401 deg
RA of node: 276
8017 deg
Eccentricity:
0017086
Arg of perigee: 126
1933 deg
Mean anomaly: 234
0805 deg
Mean motion: 15
58790572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 201
Checksum: 312
Coasting Arc #8 (Orbit 215)
---------------------------------------
Vector Time (GMT): 2012/067/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3670581
66 A = 6766359
96 meter
Y = -3286812
73 meter E =
0027262
Z = -4664412
42 I = 51
27968
XDOT = 2406
007404 Wp = 121
98367
YDOT = -6695
701542 meter/sec RA = 271
21796 deg
ZDOT = 2822
809428 TA = 176
23456
MA = 176
21401
Ha = 219
532 n
mi
Hp = 201
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12042590
74 X = -3610896
79
Y = -10783506
34 feet Y = -3327526
34 meter
Z = -15303190
36 Z = -4682098
22
XDOT = 7893
725079 XDOT = 2466
988940
YDOT = -21967
524745 feet/sec YDOT = -6668
454743 meter/sec
ZDOT = 9261
185789 ZDOT = 2834
646496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7706189
02 X = -2348846
41
Y = -14131719
69 feet Y = -4307348
16 meter
Z = -15375460
49 Z = -4686440
36
XDOT = 13636
162037 XDOT = 4156
302189
YDOT = -17572
618361 feet/sec YDOT = -5356
134076 meter/sec
ZDOT = 9310
168107 ZDOT = 2837
739239
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12067
49958234
00016717 00000-0 10270-3 0 9074
2 25544 51
6386 271
9719 0016969 129
9091 230
3559 15
58838947 2163
Satellite: ISS
Catalog Number: 25544
Epoch time: 12067
49958234 = yrday
fracday
Element set: 907
Inclination: 51
6386 deg
RA of node: 271
9719 deg
Eccentricity:
0016969
Arg of perigee: 129
9091 deg
Mean anomaly: 230
3559 deg
Mean motion: 15
58838947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 216
Checksum: 361
Coasting Arc #9 (Orbit 231)
---------------------------------------
Vector Time (GMT): 2012/068/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2251756
60 A = 6773188
31 meter
Y = 5936143
10 meter E =
0029816
Z = 2310238
84 I = 51
30387
XDOT = -4083
507152 Wp = 121
51798
YDOT = 3661
219407 meter/sec RA = 266
17358 deg
ZDOT = -5391
405200 TA = 32
49755
MA = 32
31433
Ha = 219
239 n
mi
Hp = 201
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7387652
89 X = 2173987
62
Y = 19475535
11 feet Y = 5960889
14 meter
Z = 7579523
75 Z = 2320987
88
XDOT = -13397
333176 XDOT = -4097
954255
YDOT = 12011
874696 feet/sec YDOT = 3615
473560 meter/sec
ZDOT = -17688
337271 ZDOT = -5411
278047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 838917
75 X = 255702
13
Y = 20796785
90 feet Y = 6338860
34 meter
Z = 7623186
78 Z = 2323547
33
XDOT = -14877
884030 XDOT = -4534
779052
YDOT = 7156
844218 feet/sec YDOT = 2181
406118 meter/sec
ZDOT = -17770
044452 ZDOT = -5416
309549
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12068
52529433
00016717 00000-0 10270-3 0 9085
2 25544 51
6390 266
8215 0016751 133
4885 226
7666 15
58902885 2321
Satellite: ISS
Catalog Number: 25544
Epoch time: 12068
52529433 = yrday
fracday
Element set: 908
Inclination: 51
6390 deg
RA of node: 266
8215 deg
Eccentricity:
0016751
Arg of perigee: 133
4885 deg
Mean anomaly: 226
7666 deg
Mean motion: 15
58902885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 232
Checksum: 330
Coasting Arc #10 (Orbit 247)
---------------------------------------
Vector Time (GMT): 2012/069/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -348947
65 A = 6775188
53 meter
Y = -6712149
94 meter E =
0022798
Z = 858170
62 I = 51
31211
XDOT = 4866
518499 Wp = 101
65857
YDOT = 519
614866 meter/sec RA = 261
15542 deg
ZDOT = 5905
010901 TA = 267
67943
MA = 267
94047
Ha = 219
297 n
mi
Hp = 202
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1144841
37 X = -278033
87
Y = -22021489
30 feet Y = -6715655
47 meter
Z = 2815520
42 Z = 856648
66
XDOT = 15966
268042 XDOT = 4831
661368
YDOT = 1704
773181 feet/sec YDOT = 573
841217 meter/sec
ZDOT = 19373
395346 ZDOT = 5928
567309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5461006
35 X = 1664514
74
Y = -21365080
56 feet Y = -6512076
56 meter
Z = 2809724
24 Z = 856403
95
XDOT = 13059
626835 XDOT = 3980
574259
YDOT = 5958
232400 feet/sec YDOT = 1816
069236 meter/sec
ZDOT = 19469
921984 ZDOT = 5934
432221
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12069
55098774
00016717 00000-0 10270-3 0 9099
2 25544 51
6374 261
6700 0016897 137
7023 222
5438 15
58897107 2485
Satellite: ISS
Catalog Number: 25544
Epoch time: 12069
55098774 = yrday
fracday
Element set: 909
Inclination: 51
6374 deg
RA of node: 261
6700 deg
Eccentricity:
0016897
Arg of perigee: 137
7023 deg
Mean anomaly: 222
5438 deg
Mean motion: 15
58897107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 248
Checksum: 338
Coasting Arc #11 (Orbit 262)
---------------------------------------
Vector Time (GMT): 2012/070/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1807498
99 A = 6769264
36 meter
Y = 5318550
64 meter E =
0020244
Z = -3781849
19 I = 51
29798
XDOT = -4572
749681 Wp = 125
18654
YDOT = -4513
911605 meter/sec RA = 256
12644 deg
ZDOT = -4189
923677 TA = 100
50747
MA = 100
27931
Ha = 219
126 n
mi
Hp = 202
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5930114
79 X = -1848466
44
Y = 17449313
12 feet Y = 5298108
53 meter
Z = -12407641
71 Z = -3790730
10
XDOT = -15002
459584 XDOT = -4501
580706
YDOT = -14809
421276 feet/sec YDOT = -4564
649519 meter/sec
ZDOT = -13746
468755 ZDOT = -4211
964382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10535739
35 X = -3211293
35
Y = 15090714
00 feet Y = 4599649
63 meter
Z = -12444392
70 Z = -3793050
90
XDOT = -9038
498662 XDOT = -2754
934392
YDOT = -17646
684235 feet/sec YDOT = -5378
709355 meter/sec
ZDOT = -13836
523853 ZDOT = -4217
372471
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12070
51255582
00016717 00000-0 10270-3 0 9101
2 25544 51
6371 256
8404 0016869 140
8855 219
3523 15
58930870 2637
Satellite: ISS
Catalog Number: 25544
Epoch time: 12070
51255582 = yrday
fracday
Element set: 910
Inclination: 51
6371 deg
RA of node: 256
8404 deg
Eccentricity:
0016869
Arg of perigee: 140
8855 deg
Mean anomaly: 219
3523 deg
Mean motion: 15
58930870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 263
Checksum: 312
Coasting Arc #12 (Orbit 278)
---------------------------------------
Vector Time (GMT): 2012/071/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3615273
26 A = 6763735
42 meter
Y = -2331384
23 meter E =
0020111
Z = 5210464
25 I = 51
28770
XDOT = 3151
788646 Wp = 140
71285
YDOT = 6949
756245 meter/sec RA = 251
06267 deg
ZDOT = 905
503513 TA = 300
50242
MA = 300
70083
Ha = 219
039 n
mi
Hp = 202
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11861132
75 X = 3615763
33
Y = -7648898
38 feet Y = -2290952
73 meter
Z = 17094699
00 Z = 5228028
51
XDOT = 10340
513930 XDOT = 3069
442092
YDOT = 22801
037549 feet/sec YDOT = 6984
541161 meter/sec
ZDOT = 2970
812050 ZDOT = 920
614009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13364953
01 X = 4073637
68
Y = -4254185
11 feet Y = -1296675
62 meter
Z = 17166851
50 Z = 5232456
34
XDOT = 3591
984541 XDOT = 1094
836888
YDOT = 23748
219252 feet/sec YDOT = 7238
457228 meter/sec
ZDOT = 3032
305778 ZDOT = 924
246801
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12071
53820941
00016717 00000-0 10270-3 0 9112
2 25544 51
6371 251
6891 0016875 144
6440 215
5838 15
58912804 2790
Satellite: ISS
Catalog Number: 25544
Epoch time: 12071
53820941 = yrday
fracday
Element set: 911
Inclination: 51
6371 deg
RA of node: 251
6891 deg
Eccentricity:
0016875
Arg of perigee: 144
6440 deg
Mean anomaly: 215
5838 deg
Mean motion: 15
58912804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 279
Checksum: 316
Coasting Arc #13 (Orbit 293)
---------------------------------------
Vector Time (GMT): 2012/072/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4710807
68 A = 6765783
31 meter
Y = -1335279
18 meter E =
0026338
Z = -4693984
56 I = 51
30623
XDOT = -744
370298 Wp = 133
27612
YDOT = -7102
604442 meter/sec RA = 245
98764 deg
ZDOT = 2759
567409 TA = 164
26863
MA = 164
18664
Ha = 218
948 n
mi
Hp = 202
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15455405
76 X = -4672723
90
Y = -4380837
21 feet Y = -1387745
78 meter
Z = -15400211
82 Z = -4716776
82
XDOT = -2442
159769 XDOT = -678
297565
YDOT = -23302
508012 feet/sec YDOT = -7110
558799 meter/sec
ZDOT = 9053
698847 ZDOT = 2756
112346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13789062
86 X = -4202906
36
Y = -8064677
78 feet Y = -2458113
79 meter
Z = -15493564
60 Z = -4722438
49
XDOT = 2788
853834 XDOT = 850
042649
YDOT = -22185
331473 feet/sec YDOT = -6762
089033 meter/sec
ZDOT = 9039
991003 ZDOT = 2755
389258
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12072
49973769
00016717 00000-0 10270-3 0 9126
2 25544 51
6371 246
8590 0016937 148
3578 211
8599 15
58987181 2944
Satellite: ISS
Catalog Number: 25544
Epoch time: 12072
49973769 = yrday
fracday
Element set: 912
Inclination: 51
6371 deg
RA of node: 246
8590 deg
Eccentricity:
0016937
Arg of perigee: 148
3578 deg
Mean anomaly: 211
8599 deg
Mean motion: 15
58987181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 294
Checksum: 364
Coasting Arc #14 (Orbit 309)
---------------------------------------
Vector Time (GMT): 2012/073/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4572941
58 A = 6772741
22 meter
Y = 4391409
94 meter E =
0028157
Z = 2331113
82 I = 51
34336
XDOT = -2111
367141 Wp = 131
98958
YDOT = 5069
727724 meter/sec RA = 240
94414 deg
ZDOT = -5385
383529 TA = 21
78426
MA = 21
66475
Ha = 218
615 n
mi
Hp = 202
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15003089
18 X = 4512172
09
Y = 14407512
91 feet Y = 4442207
75 meter
Z = 7648011
23 Z = 2353181
02
XDOT = -6927
057550 XDOT = -2141
740045
YDOT = 16632
964974 feet/sec YDOT = 5045
946970 meter/sec
ZDOT = -17668
581132 ZDOT = -5395
714495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11205308
93 X = 3415378
16
Y = 17484920
13 feet Y = 5329403
66 meter
Z = 7738204
51 Z = 2358604
73
XDOT = -9217
407301 XDOT = -2809
465745
YDOT = 13778
738445 feet/sec YDOT = 4199
759478 meter/sec
ZDOT = -17711
260556 ZDOT = -5398
392217
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12073
52534704
00016717 00000-0 10270-3 0 9134
2 25544 51
6372 241
7080 0016708 152
5400 207
6641 15
59032391 3105
Satellite: ISS
Catalog Number: 25544
Epoch time: 12073
52534704 = yrday
fracday
Element set: 913
Inclination: 51
6372 deg
RA of node: 241
7080 deg
Eccentricity:
0016708
Arg of perigee: 152
5400 deg
Mean anomaly: 207
6641 deg
Mean motion: 15
59032391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 310
Checksum: 273
Coasting Arc #15 (Orbit 325)
---------------------------------------
Vector Time (GMT): 2012/074/11:43:29
451
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3147526
61 A = 6774691
71 meter
Y = -5935033
09 meter E =
0019429
Z = 897850
83 I = 51
36586
XDOT = 4642
906892 Wp = 113
23564
YDOT = -1553
105105 meter/sec RA = 235
92958 deg
ZDOT = 5900
439084 TA = 256
52802
MA = 256
74460
Ha = 218
653 n
mi
Hp = 202
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10326530
86 X = -3085287
46
Y = -19471893
35 feet Y = -5969882
64 meter
Z = 2945704
82 Z = 882711
87
XDOT = 15232
634159 XDOT = 4631
266159
YDOT = -5095
489191 feet/sec YDOT = -1501
250052 meter/sec
ZDOT = 19358
395944 ZDOT = 5922
965752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5910419
96 X = -1801496
00
Y = -21241904
30 feet Y = -6474532
43 meter
Z = 2884004
98 Z = 879044
72
XDOT = 14308
037103 XDOT = 4361
089709
YDOT = -1290
506051 feet/sec YDOT = -393
346244 meter/sec
ZDOT = 19450
860144 ZDOT = 5928
622172
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12074
55093630
00016717 00000-0 10270-3 0 9147
2 25544 51
6372 236
5567 0016907 156
0647 204
1298 15
59062108 3266
Satellite: ISS
Catalog Number: 25544
Epoch time: 12074
55093630 = yrday
fracday
Element set: 914
Inclination: 51
6372 deg
RA of node: 236
5567 deg
Eccentricity:
0016907
Arg of perigee: 156
0647 deg
Mean anomaly: 204
1298 deg
Mean motion: 15
59062108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 326
Checksum: 307
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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